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Air at 7.8 bar and 180 C expands through a convergent divergent nozzle into a space at 1.03 bar. The flow rate of air is 3.6 kg/s. Assuming isentropic flow through out and neglecting the inlet velocity, calculate the throat and exit areas of the nozzle.

Question-Answer › Category: Fluid Mechanics › Air at 7.8 bar and 180 C expands through a convergent divergent nozzle into a space at 1.03 bar. The flow rate of air is 3.6 kg/s. Assuming isentropic flow through out and neglecting the inlet velocity, calculate the throat and exit areas of the nozzle.
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Suresh asked 10 months ago
Air at 7.8 bar and 180 C expands through a convergent divergent nozzle into a space at 1.03 bar. The flow rate of air is 3.6 kg/s. Assuming isentropic flow through out and neglecting the inlet velocity, calculate the throat and exit areas of the nozzle.
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Mazurek Gravity Staff answered 10 months ago

 
 

103bar P 127.860s/ 12 2 180 en p7316603 fromila 20528 Pe Concello (15-4)Grob Pc 20.528 → Per 0.5288 7.82 4.11 84 bas PL Also,
poofect gas equation 14-1 (-2/A 7.8 14 TA 1:03 P2 > 254.02% 2 1.783 > T, > 953 11.783 Tz re RT2 28 7x 2540 2 1:03 x105 30:707
 

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